Segmentation-based super-low altitude flight control method for pilotless aircraft

A low-altitude flight, control method technology, applied in attitude control, non-electric variable control, control/regulation system, etc., can solve problems such as large step response, high fuel consumption, and increased cost

Active Publication Date: 2019-03-29
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS +2
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The traditional control mode of the longitudinal channel of the UAV is to adjust the elevator rudder surface by measuring the pitch angle and the pitch angle rate to realize the UAV glide and attitude maintenance, but the height control error of this strategy is large and the mode between modes The switching is not smooth enough and the step response is large, which is not conducive to ultra-low altitude flight
At present, in response to the difficulty of ultra-low-altitude flight control of UAVs, research institutions at home and abroad mainly install laser height sensors with centimeter-level accuracy, and use the measured relative heights to directly participate in the control to improve the height control accuracy, but the cost

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  • Segmentation-based super-low altitude flight control method for pilotless aircraft
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  • Segmentation-based super-low altitude flight control method for pilotless aircraft

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Embodiment Construction

[0065] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments. The following examples are only used to illustrate the technical solution of the present invention more clearly, but not to limit the protection scope of the present invention.

[0066] UAV ultra-low-altitude flight control working principle: the working principle of the ultra-low-altitude flight control system in the specific embodiment of the present invention is as follows figure 1 As shown, the system needs sensors (gyro platform, angular rate gyro, radio altimeter) to measure the flight state of the UAV (pitch angle, roll angle, pitch angle rate, relative flight altitude), and then the flight control computer according to the preset instructions Perform comparison calculations, and output control signals to the actuator (elevator steering gear) to drive the steering surface (elevator rudder surface), thereby generating aerodynamic force / mome...

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Abstract

The invention discloses a segmentation-based super-low altitude flight control method for a pilotless aircraft. The method comprises the steps of: judging the flight mode of the pilotless aircraft according to a preset flight mode judging condition of the pilotless aircraft, wherein the flight mode is divided into super-low altitude flight mode, super-low altitude level-off flight mode, and super-low altitude quitting flight mode; determining the longitudinal segmented flight control strategy of the pilotless aircraft in the super-low altitude flight mode according to the judgment result, anddesigning the longitudinal segmented control law of the pilotless aircraft; and refining specific control logic and control law parameters. According to the segmentation-based super-low altitude flight control method for the pilotless aircraft, the pilotless aircraft can enters super-low altitude flight mode in a relatively stable posture under a small disturbance environment; the flight range isshortened, and the oil consumption is reduced; and after the pilotless aircraft quits the super-low altitude flight, the pilotless aircraft can climb at the maximum dynamic pressure with an allowed overload, and then enters a second super-low altitude flight or returns.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicle flight control, in particular to a subsection-based ultra-low-altitude flight control method for unmanned aerial vehicles. Background technique [0002] Ultra-low-altitude flight is a kind of tactical flight widely used in the world at present, and it has good concealment and suddenness. Ultra-low-altitude penetration tactics and technologies began during the Second World War. In the past 20 to 30 years, they have developed by leaps and bounds. , anti-tank missiles, ground attack missiles, and unmanned aerial vehicles are the most eye-catching. Applying ultra-low-altitude flight to unmanned aerial vehicles can greatly improve the concealment and maneuverability of unmanned aerial vehicles, and can achieve the greatest combat results at a relatively small cost, realizing a strategic combat style. [0003] The ultra-low-altitude flight of UAVs can conceal itself and has the incomparable supe...

Claims

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Application Information

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IPC IPC(8): G05D1/08G05D1/10
CPCG05D1/0808G05D1/101
Inventor 刘蓉高艳辉李志宇吴在桂郭剑东
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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